Path: Interplanetary/LowEnergyManeuver
% Demonstrate low-energy transfer targeting for a 3-body system Start with an initial orbit and impulsive burn, then numerically optimize so that the location of the Moon is the final condition and the magnitude of the burn is minimized. The dynamical model is the 3 body problem, but functions exist also for the CRTBP and the full 4 body problem. % See also PlanetId, PlanetPositionEMBarycenter, PlotLET3BP, Targeting3BP2 LowEnergyTransferInCRTBP Targeting4BP
Interplanetary: Ephemeris/PlanetPositionEMBarycenter Interplanetary: LowEnergyManeuver/PlanetId Interplanetary: LowEnergyManeuver/PlotLET3BP Interplanetary: LowEnergyManeuver/Targeting3BP2
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